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    Automatic Optimization of Preswirl Nozzle Design

    Source: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 002::page 387
    Author:
    Fabio Ciampoli
    ,
    Shahrokh Shahpar
    ,
    Elisabeth Willocq
    ,
    John W. Chew
    DOI: 10.1115/1.2364194
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The objective of the research described here is to develop and demonstrate use of automatic design methods for preswirl nozzles. Performance of preswirled cooling air delivery systems depends critically on the design of these nozzles which is subject to manufacturing and stress constraints. The best solution may be a compromise between cost and performance. Here it is shown that automatic optimization using computational fluid dynamics (CFD) to evaluate nozzle performance can be useful in design. A parametric geometric model of a nozzle with appropriate constraints is first defined and the CFD meshing and solution are then automated. The mesh generation is found to be the most delicate task in the whole process. Direct hill climbing (DHC) and response surface model (RSM) optimization methods have been evaluated. For the test case considered, significant nozzle performance improvements were obtained using both methods, but the RSM model was preferred.
    keyword(s): Computational fluid dynamics , Design , Nozzles , Optimization , Geometry AND Response surface methodology ,
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      Automatic Optimization of Preswirl Nozzle Design

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    http://yetl.yabesh.ir/yetl1/handle/yetl/135735
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    contributor authorFabio Ciampoli
    contributor authorShahrokh Shahpar
    contributor authorElisabeth Willocq
    contributor authorJohn W. Chew
    date accessioned2017-05-09T00:23:43Z
    date available2017-05-09T00:23:43Z
    date copyrightApril, 2007
    date issued2007
    identifier issn1528-8919
    identifier otherJETPEZ-26949#387_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135735
    description abstractThe objective of the research described here is to develop and demonstrate use of automatic design methods for preswirl nozzles. Performance of preswirled cooling air delivery systems depends critically on the design of these nozzles which is subject to manufacturing and stress constraints. The best solution may be a compromise between cost and performance. Here it is shown that automatic optimization using computational fluid dynamics (CFD) to evaluate nozzle performance can be useful in design. A parametric geometric model of a nozzle with appropriate constraints is first defined and the CFD meshing and solution are then automated. The mesh generation is found to be the most delicate task in the whole process. Direct hill climbing (DHC) and response surface model (RSM) optimization methods have been evaluated. For the test case considered, significant nozzle performance improvements were obtained using both methods, but the RSM model was preferred.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAutomatic Optimization of Preswirl Nozzle Design
    typeJournal Paper
    journal volume129
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2364194
    journal fristpage387
    journal lastpage393
    identifier eissn0742-4795
    keywordsComputational fluid dynamics
    keywordsDesign
    keywordsNozzles
    keywordsOptimization
    keywordsGeometry AND Response surface methodology
    treeJournal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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